+ All Categories
Home > Documents > NREL Phase VI - Test Blade & Aerofoil Geometry

NREL Phase VI - Test Blade & Aerofoil Geometry

Date post: 22-Oct-2014
Category:
Upload: jay-avraj-bhatti
View: 188 times
Download: 5 times
Share this document with a friend
Popular Tags:
44
GEOMETRY 0.000 SS1 0.000 0.218 0.000 0.2180 50.0 0.1090 0.508 SS2 0.101 0.218 0.000 0.2180 50.0 0.1090 0.660 SS3 0.131 0.218 0.000 0.2180 50.0 0.1090 0.883 SS4 0.176 0.183 0.000 0.1830 50.0 0.0915 1.008 SS5 0.200 0.349 6.700 0.1630 35.9 0.1253 1.067 SS6 0.212 0.441 9.900 0.1540 33.5 0.1477 1.133 SS7 0.225 0.544 13.400 0.1540 31.9 0.1735 1.257 SS8 0.250 0.737 20.040 0.1540 30.0 0.2211 1.343 SS9 0.267 0.728 18.074 0.1525 30.0 0.2184 1.510 SS10 0.300 0.711 14.292 0.1490 30.0 0.2133 1.648 SS11 0.328 0.697 11.909 0.1460 30.0 0.2091 1.952 SS12 0.388 0.666 7.979 0.1395 30.0 0.1998 2.257 SS13 0.449 0.636 5.308 0.1332 30.0 0.1908 2.343 SS14 0.466 0.627 4.715 0.1314 30.0 0.1881 2.562 SS15 0.509 0.605 3.425 0.1267 30.0 0.1815 2.867 SS16 0.570 0.574 2.083 0.1203 30.0 0.1722 3.172 SS17 0.631 0.543 1.150 0.1138 30.0 0.1629 3.185 SS18 0.633 0.542 1.115 0.1135 30.0 0.1626 3.476 SS19 0.691 0.512 0.494 0.1073 30.0 0.1536 3.781 SS20 0.752 0.482 -0.015 0.1010 30.0 0.1446 4.023 SS21 0.800 0.457 -0.381 0.0957 30.0 0.1371 4.086 SS22 0.812 0.451 -0.475 0.0945 30.0 0.1353 4.391 SS23 0.873 0.420 -0.920 0.0880 30.0 0.1260 4.696 SS24 0.934 0.389 -1.352 0.0815 30.0 0.1167 4.780 SS25 0.950 0.381 -1.469 0.0798 30.0 0.1143 5.000 SS26 0.994 0.358 -1.775 0.0750 30.0 0.1074 Radial Distance (m) Station Number Span Station (r/5.029 m) Chord Length (m) Twist (degrees) Thickness (m) Twist Axis (% chord) Twist Position (x in m)
Transcript
Page 1: NREL Phase VI - Test Blade & Aerofoil Geometry

GEOMETRY

0.000 SS1 0.000 0.218 0.000 0.2180 50.0 0.10900.508 SS2 0.101 0.218 0.000 0.2180 50.0 0.10900.660 SS3 0.131 0.218 0.000 0.2180 50.0 0.10900.883 SS4 0.176 0.183 0.000 0.1830 50.0 0.09151.008 SS5 0.200 0.349 6.700 0.1630 35.9 0.12531.067 SS6 0.212 0.441 9.900 0.1540 33.5 0.14771.133 SS7 0.225 0.544 13.400 0.1540 31.9 0.17351.257 SS8 0.250 0.737 20.040 0.1540 30.0 0.22111.343 SS9 0.267 0.728 18.074 0.1525 30.0 0.21841.510 SS10 0.300 0.711 14.292 0.1490 30.0 0.21331.648 SS11 0.328 0.697 11.909 0.1460 30.0 0.20911.952 SS12 0.388 0.666 7.979 0.1395 30.0 0.19982.257 SS13 0.449 0.636 5.308 0.1332 30.0 0.19082.343 SS14 0.466 0.627 4.715 0.1314 30.0 0.18812.562 SS15 0.509 0.605 3.425 0.1267 30.0 0.18152.867 SS16 0.570 0.574 2.083 0.1203 30.0 0.17223.172 SS17 0.631 0.543 1.150 0.1138 30.0 0.16293.185 SS18 0.633 0.542 1.115 0.1135 30.0 0.16263.476 SS19 0.691 0.512 0.494 0.1073 30.0 0.15363.781 SS20 0.752 0.482 -0.015 0.1010 30.0 0.14464.023 SS21 0.800 0.457 -0.381 0.0957 30.0 0.13714.086 SS22 0.812 0.451 -0.475 0.0945 30.0 0.13534.391 SS23 0.873 0.420 -0.920 0.0880 30.0 0.12604.696 SS24 0.934 0.389 -1.352 0.0815 30.0 0.11674.780 SS25 0.950 0.381 -1.469 0.0798 30.0 0.11435.000 SS26 0.994 0.358 -1.775 0.0750 30.0 0.1074

Radial Distance(m)

Station Number

SpanStation

(r/5.029 m)Chord Length

(m)Twist

(degrees)Thickness

(m)Twist Axis(% chord)

Twist Position(x in m)

A3
Aeronautics: The root of the Blade is assumed to be a clamped joint attached to a shaft, rotating about the global Y-Axis
A4
Aeronautics: Blade Root Area - blade geometry converges to a cylinder just before attachment to shaft
G4
Aeronautics: Axis of rotation at 50% of the chord at this station indicates the rotation is about the longitudinal axis of the blade
A6
Aeronautics: Grey shade to indicate transition between the Blade Root and first Aerofoil Station
A10
Aeronautics: First station at which the the S809 Aerofoil shape is maintained through the entirety of the blade span
G10
Aeronautics: The twist axis is maintained at 30% of chord for the Blade section of the turbine
A12
Aeronautics: Pressure Station 30.0%
A16
Aeronautics: Pressure Station 46.6%
A23
Aeronautics: Pressure Station 80%
A27
Aeronautics: Pressure Station 95%
Page 2: NREL Phase VI - Test Blade & Aerofoil Geometry

Upper Surface Lower Surface ORIGINALx/c y/c x/c y/c

0.000370 0.002750 0.001400 -0.0049800.005750 0.011660 0.009330 -0.0127200.016260 0.021330 0.023210 -0.0216200.031580 0.031360 0.042230 -0.0314400.051470 0.041430 0.065790 -0.0419900.075680 0.051320 0.093250 -0.0530100.103900 0.060820 0.123970 -0.0640800.135800 0.069720 0.157520 -0.0746700.171030 0.077860 0.193620 -0.0844700.209200 0.085050 0.231750 -0.0932600.249870 0.091130 0.271290 -0.1006000.292590 0.095940 0.311880 -0.1058900.336890 0.099330 0.353280 -0.1086600.382230 0.101090 0.395410 -0.1084200.428090 0.101010 0.438320 -0.1048400.473840 0.098430 0.482340 -0.0975600.520050 0.092370 0.528370 -0.0869700.568010 0.083560 0.576630 -0.0744200.617470 0.073790 0.626490 -0.0611200.667180 0.064030 0.677100 -0.0479200.716060 0.054620 0.727520 -0.0355800.763140 0.045780 0.776680 -0.0246600.807560 0.037610 0.823480 -0.0155900.848540 0.030170 0.866770 -0.0085900.885370 0.023350 0.905450 -0.0037000.917630 0.016940 0.938520 -0.0007500.945230 0.011010 0.965090 0.0005400.967990 0.006000 0.984460 0.0006500.985280 0.002450 0.996120 0.0002400.996230 0.000540 1.000000 0.0000001.000000 0.000000

R = 1.257 0.737 S8Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.27 2.03 1.03 -3.67 0.27269,2.026754.24 8.59 6.88 -9.37 4.23775,8.59342

11.98 15.72 17.11 -15.93 11.98362,15.7202123.27 23.11 31.12 -23.17 23.27446,23.1123237.93 30.53 48.49 -30.95 37.93339,30.5339155.78 37.82 68.73 -39.07 55.77616,37.8228476.57 44.82 91.37 -47.23 76.5743,44.82434

100.08 51.38 116.09 -55.03 100.0846,51.38364126.05 57.38 142.70 -62.25 126.04911,57.38282154.18 62.68 170.80 -68.73 154.1804,62.68185184.15 67.16 199.94 -74.14 184.15419,67.16281215.64 70.71 229.86 -78.04 215.63883,70.70778248.29 73.21 260.37 -80.08 248.28793,73.20621281.70 74.50 291.42 -79.91 281.70351,74.50333315.50 74.44 323.04 -77.27 315.50233,74.44437349.22 72.54 355.48 -71.90 349.22008,72.54291383.28 68.08 389.41 -64.10 383.27685,68.07669

Page 3: NREL Phase VI - Test Blade & Aerofoil Geometry

418.62 61.58 424.98 -54.85 418.62337,61.58372455.08 54.38 461.72 -45.05 455.07539,54.38323491.71 47.19 499.02 -35.32 491.71166,47.19011527.74 40.25 536.18 -26.22 527.73622,40.25494562.43 33.74 572.41 -18.17 562.43418,33.73986595.17 27.72 606.90 -11.49 595.17172,27.71857625.37 22.24 638.81 -6.33 625.37398,22.23529652.52 17.21 667.32 -2.73 652.51769,17.20895676.29 12.48 691.69 -0.55 676.29331,12.48478696.63 8.11 711.27 0.40 696.63451,8.11437713.41 4.42 725.55 0.48 713.40863,4.422726.15 1.81 734.14 0.18 726.15136,1.80565734.22 0.40 736.85 -0.15 734.22151,0.39798736.85 0.15 737.00 0.00 736.8526,0.1474

R = 1.343 c = 0.728 S9Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.27 2.00 1.02 -3.63 0.26936,2.0024.19 8.49 6.79 -9.26 4.186,8.48848

11.84 15.53 16.90 -15.74 11.83728,15.5282422.99 22.83 30.74 -22.89 22.99024,22.8300837.47 30.16 47.90 -30.57 37.47016,30.1610455.10 37.36 67.89 -38.59 55.09504,37.3609675.64 44.28 90.25 -46.65 75.6392,44.2769698.86 50.76 114.67 -54.36 98.8624,50.75616

124.51 56.68 140.96 -61.49 124.50984,56.68208152.30 61.92 168.71 -67.89 152.2976,61.9164181.91 66.34 197.50 -73.24 181.90536,66.34264213.01 69.84 227.05 -77.09 213.00552,69.84432245.26 72.31 257.19 -79.10 245.25592,72.31224278.26 73.59 287.86 -78.93 278.26344,73.59352311.65 73.54 319.10 -76.32 311.64952,73.53528344.96 71.66 351.14 -71.02 344.95552,71.65704378.60 67.25 384.65 -63.31 378.5964,67.24536413.51 60.83 419.79 -54.18 413.51128,60.83168449.52 53.72 456.08 -44.50 449.51816,53.71912485.71 46.61 492.93 -34.89 485.70704,46.61384521.29 39.76 529.63 -25.90 521.29168,39.76336555.57 33.33 565.42 -17.95 555.56592,33.32784587.90 27.38 599.49 -11.35 587.90368,27.38008617.74 21.96 631.01 -6.25 617.73712,21.96376644.55 17.00 659.17 -2.69 644.54936,16.9988668.03 12.33 683.24 -0.55 668.03464,12.33232688.13 8.02 702.59 0.39 688.12744,8.01528704.70 4.37 716.69 0.47 704.69672,4.368717.28 1.78 725.18 0.17 717.28384,1.7836725.26 0.39 727.93 -0.07 725.25544,0.39312727.93 0.07 728.00 0.00 727.9272,0.0728

R = 1.510 c = 0.711 S10Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.26 1.96 1.00 -3.54 0.26307,1.95525

Page 4: NREL Phase VI - Test Blade & Aerofoil Geometry

4.09 8.29 6.63 -9.04 4.08825,8.2902611.56 15.17 16.50 -15.37 11.56086,15.1656322.45 22.30 30.03 -22.35 22.45338,22.2969636.60 29.46 46.78 -29.85 36.59517,29.4567353.81 36.49 66.30 -37.69 53.80848,36.4885273.87 43.24 88.14 -45.56 73.8729,43.2430296.55 49.57 112.00 -53.09 96.5538,49.57092

121.60 55.36 137.66 -60.06 121.60233,55.35846148.74 60.47 164.77 -66.31 148.7412,60.47055177.66 64.79 192.89 -71.53 177.65757,64.79343208.03 68.21 221.75 -75.29 208.03149,68.21334239.53 70.62 251.18 -77.26 239.52879,70.62363271.77 71.87 281.14 -77.09 271.76553,71.87499304.37 71.82 311.65 -74.54 304.37199,71.81811336.90 69.98 342.94 -69.37 336.90024,69.98373369.76 65.68 375.67 -61.84 369.75555,65.67507403.86 59.41 409.98 -52.91 403.85511,59.41116439.02 52.46 445.43 -43.46 439.02117,52.46469474.36 45.53 481.42 -34.07 474.36498,45.52533509.12 38.83 517.27 -25.30 509.11866,38.83482542.59 32.55 552.22 -17.53 542.59254,32.54958574.18 26.74 585.49 -11.08 574.17516,26.74071603.31 21.45 616.27 -6.11 603.31194,21.45087629.50 16.60 643.77 -2.63 629.49807,16.60185652.43 12.04 667.29 -0.53 652.43493,12.04434672.06 7.83 686.18 0.38 672.05853,7.82811688.24 4.27 699.95 0.46 688.24089,4.266700.53 1.74 708.24 0.17 700.53408,1.74195708.32 0.38 710.93 -0.07 708.31953,0.38394710.93 0.07 711.00 0.00 710.9289,0.0711

R = 1.648 c = 0.697 S11Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.26 1.92 0.98 -3.47 0.25789,1.916754.01 8.13 6.50 -8.87 4.00775,8.12702

11.33 14.87 16.18 -15.07 11.33322,14.8670122.01 21.86 29.43 -21.91 22.01126,21.8579235.87 28.88 45.86 -29.27 35.87459,28.8767152.75 35.77 65.00 -36.95 52.74896,35.7700472.42 42.39 86.41 -44.66 72.4183,42.3915494.65 48.59 109.79 -52.04 94.6526,48.59484

119.21 54.27 134.95 -58.88 119.20791,54.26842145.81 59.28 161.53 -65.00 145.8124,59.27985174.16 63.52 189.09 -70.12 174.15939,63.51761203.94 66.87 217.38 -73.81 203.93523,66.87018234.81 69.23 246.24 -75.74 234.81233,69.23301266.41 70.46 275.60 -75.57 266.41431,70.45973298.38 70.40 305.51 -73.07 298.37873,70.40397330.27 68.61 336.19 -68.00 330.26648,68.60571362.47 64.38 368.27 -60.62 362.47485,64.38189395.90 58.24 401.91 -51.87 395.90297,58.24132430.38 51.43 436.66 -42.60 430.37659,51.43163465.02 44.63 471.94 -33.40 465.02446,44.62891

Page 5: NREL Phase VI - Test Blade & Aerofoil Geometry

499.09 38.07 507.08 -24.80 499.09382,38.07014531.91 31.91 541.35 -17.19 531.90858,31.90866562.87 26.21 573.97 -10.87 562.86932,26.21417591.43 21.03 604.14 -5.99 591.43238,21.02849617.10 16.27 631.10 -2.58 617.10289,16.27495639.59 11.81 654.15 -0.52 639.58811,11.80718658.83 7.67 672.67 0.38 658.82531,7.67397674.69 4.18 686.17 0.45 674.68903,4.182686.74 1.71 694.30 0.17 686.74016,1.70765694.37 0.38 696.93 -0.07 694.37231,0.37638696.93 0.07 697.00 0.00 696.9303,0.0697

R = 1.952 c = 0.666 S12Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.25 1.83 0.93 -3.32 0.24642,1.83153.83 7.77 6.21 -8.47 3.8295,7.76556

10.83 14.21 15.46 -14.40 10.82916,14.2057821.03 20.89 28.13 -20.94 21.03228,20.8857634.28 27.59 43.82 -27.97 34.27902,27.5923850.40 34.18 62.10 -35.30 50.40288,34.1791269.20 40.51 82.56 -42.68 69.1974,40.5061290.44 46.43 104.91 -49.73 90.4428,46.43352

113.91 51.85 128.95 -56.26 113.90598,51.85476139.33 56.64 154.35 -62.11 139.3272,56.6433166.41 60.69 180.68 -67.00 166.41342,60.69258194.86 63.90 207.71 -70.52 194.86494,63.89604224.37 66.15 235.28 -72.37 224.36874,66.15378254.57 67.33 263.34 -72.21 254.56518,67.32594285.11 67.27 291.92 -69.82 285.10794,67.27266315.58 65.55 321.24 -64.97 315.57744,65.55438346.35 61.52 351.89 -57.92 346.3533,61.51842378.29 55.65 384.04 -49.56 378.29466,55.65096411.24 49.14 417.24 -40.71 411.23502,49.14414444.34 42.64 450.95 -31.91 444.34188,42.64398476.90 36.38 484.53 -23.70 476.89596,36.37692508.25 30.49 517.27 -16.42 508.25124,30.48948537.83 25.05 548.44 -10.38 537.83496,25.04826565.13 20.09 577.27 -5.72 565.12764,20.09322589.66 15.55 603.03 -2.46 589.65642,15.5511611.14 11.28 625.05 -0.50 611.14158,11.28204629.52 7.33 642.75 0.36 629.52318,7.33266644.68 4.00 655.65 0.43 644.68134,3.996656.20 1.63 663.42 0.16 656.19648,1.6317663.49 0.36 665.93 -0.07 663.48918,0.35964665.93 0.07 666.00 0.00 665.9334,0.0666

R = 2.257 c = 0.636 S13Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.24 1.75 0.89 -3.17 0.23532,1.7493.66 7.42 5.93 -8.09 3.657,7.41576

10.34 13.57 14.76 -13.75 10.34136,13.5658820.08 19.94 26.86 -20.00 20.08488,19.94496

Page 6: NREL Phase VI - Test Blade & Aerofoil Geometry

32.73 26.35 41.84 -26.71 32.73492,26.3494848.13 32.64 59.31 -33.71 48.13248,32.6395266.08 38.68 78.84 -40.75 66.0804,38.6815286.37 44.34 100.18 -47.49 86.3688,44.34192

108.78 49.52 123.14 -53.72 108.77508,49.51896133.05 54.09 147.39 -59.31 133.0512,54.0918158.92 57.96 172.54 -63.98 158.91732,57.95868186.09 61.02 198.36 -67.35 186.08724,61.01784214.26 63.17 224.69 -69.11 214.26204,63.17388243.10 64.29 251.48 -68.96 243.09828,64.29324272.27 64.24 278.77 -66.68 272.26524,64.24236301.36 62.60 306.77 -62.05 301.36224,62.60148330.75 58.75 336.04 -55.31 330.7518,58.74732361.25 53.14 366.74 -47.33 361.25436,53.14416392.71 46.93 398.45 -38.87 392.71092,46.93044424.33 40.72 430.64 -30.48 424.32648,40.72308455.41 34.74 462.70 -22.63 455.41416,34.73832485.36 29.12 493.97 -15.68 485.35704,29.11608513.61 23.92 523.73 -9.92 513.60816,23.91996539.67 19.19 551.27 -5.46 539.67144,19.18812563.10 14.85 575.87 -2.35 563.09532,14.8506583.61 10.77 596.90 -0.48 583.61268,10.77384601.17 7.00 613.80 0.34 601.16628,7.00236615.64 3.82 626.12 0.41 615.64164,3.816626.64 1.56 633.53 0.15 626.63808,1.5582633.60 0.34 635.94 -0.06 633.60228,0.34344635.94 0.06 636.00 0.00 635.9364,0.0636

R = 2.343 c = 0.627 S14Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.23 1.72 0.88 -3.12 0.23199,1.724253.61 7.31 5.85 -7.98 3.60525,7.31082

10.20 13.37 14.55 -13.56 10.19502,13.3739119.80 19.66 26.48 -19.71 19.80066,19.6627232.27 25.98 41.25 -26.33 32.27169,25.9766147.45 32.18 58.47 -33.24 47.45136,32.1776465.15 38.13 77.73 -40.18 65.1453,38.1341485.15 43.71 98.77 -46.82 85.1466,43.71444

107.24 48.82 121.40 -52.96 107.23581,48.81822131.17 53.33 145.31 -58.47 131.1684,53.32635156.67 57.14 170.10 -63.08 156.66849,57.13851183.45 60.15 195.55 -66.39 183.45393,60.15438211.23 62.28 221.51 -68.13 211.23003,62.27991239.66 63.38 247.92 -67.98 239.65821,63.38343268.41 63.33 274.83 -65.73 268.41243,63.33327297.10 61.72 302.43 -61.17 297.09768,61.71561326.07 57.92 331.29 -54.53 326.07135,57.91599356.14 52.39 361.55 -46.66 356.14227,52.39212387.15 46.27 392.81 -38.32 387.15369,46.26633418.32 40.15 424.54 -30.05 418.32186,40.14681448.97 34.25 456.16 -22.31 448.96962,34.24674478.49 28.70 486.98 -15.46 478.48878,28.70406506.34 23.58 516.32 -9.77 506.34012,23.58147

Page 7: NREL Phase VI - Test Blade & Aerofoil Geometry

532.03 18.92 543.46 -5.39 532.03458,18.91659555.13 14.64 567.72 -2.32 555.12699,14.64045575.35 10.62 588.45 -0.47 575.35401,10.62138592.66 6.90 605.11 0.34 592.65921,6.90327606.93 3.76 617.26 0.41 606.92973,3.762617.77 1.54 624.57 0.15 617.77056,1.53615624.64 0.34 626.94 -0.06 624.63621,0.33858626.94 0.06 627.00 0.00 626.9373,0.0627

R = 2.562 c = 0.605 S15Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.22 1.66 0.85 -3.01 0.22385,1.663753.48 7.05 5.64 -7.70 3.47875,7.05439.84 12.90 14.04 -13.08 9.8373,12.90465

19.11 18.97 25.55 -19.02 19.1059,18.972831.14 25.07 39.80 -25.40 31.13935,25.0651545.79 31.05 56.42 -32.07 45.7864,31.048662.86 36.80 75.00 -38.77 62.8595,36.796182.16 42.18 95.30 -45.18 82.159,42.1806

103.47 47.11 117.14 -51.10 103.47315,47.1053126.57 51.46 140.21 -56.42 126.566,51.45525151.17 55.13 164.13 -60.86 151.17135,55.13365177.02 58.04 188.69 -64.06 177.01695,58.0437203.82 60.09 213.73 -65.74 203.81845,60.09465231.25 61.16 239.22 -65.59 231.24915,61.15945258.99 61.11 265.18 -63.43 258.99445,61.11105286.67 59.55 291.82 -59.02 286.6732,59.55015314.63 55.88 319.66 -52.62 314.63025,55.88385343.65 50.55 348.86 -45.02 343.64605,50.5538373.57 44.64 379.03 -36.98 373.56935,44.64295403.64 38.74 409.65 -28.99 403.6439,38.73815433.22 33.05 440.15 -21.53 433.2163,33.0451461.70 27.70 469.89 -14.92 461.6997,27.6969488.57 22.75 498.21 -9.43 488.5738,22.75405513.37 18.25 524.40 -5.20 513.3667,18.25285535.65 14.13 547.80 -2.24 535.64885,14.12675555.17 10.25 567.80 -0.45 555.16615,10.2487571.86 6.66 583.88 0.33 571.86415,6.66105585.63 3.63 595.60 0.39 585.63395,3.63596.09 1.48 602.65 0.15 596.0944,1.48225602.72 0.33 604.94 -0.06 602.71915,0.3267604.94 0.06 605.00 0.00 604.9395,0.0605

R = 2.867 c = 0.574 S16Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.21 1.58 0.80 -2.86 0.21238,1.57853.30 6.69 5.36 -7.30 3.3005,6.692849.33 12.24 13.32 -12.41 9.33324,12.24342

18.13 18.00 24.24 -18.05 18.12692,18.0006429.54 23.78 37.76 -24.10 29.54378,23.7808243.44 29.46 53.53 -30.43 43.44032,29.4576859.64 34.91 71.16 -36.78 59.6386,34.91068

Page 8: NREL Phase VI - Test Blade & Aerofoil Geometry

77.95 40.02 90.42 -42.86 77.9492,40.0192898.17 44.69 111.14 -48.49 98.17122,44.69164

120.08 48.82 133.02 -53.53 120.0808,48.8187143.43 52.31 155.72 -57.74 143.42538,52.30862167.95 55.07 179.02 -60.78 167.94666,55.06956193.37 57.02 202.78 -62.37 193.37486,57.01542219.40 58.03 226.97 -62.23 219.40002,58.02566245.72 57.98 251.60 -60.18 245.72366,57.97974271.98 56.50 276.86 -56.00 271.98416,56.49882298.51 53.02 303.28 -49.92 298.5087,53.02038326.04 47.96 330.99 -42.72 326.03774,47.96344354.43 42.36 359.61 -35.08 354.42778,42.35546382.96 36.75 388.66 -27.51 382.96132,36.75322411.02 31.35 417.60 -20.42 411.01844,31.35188438.04 26.28 445.81 -14.15 438.04236,26.27772463.54 21.59 472.68 -8.95 463.53944,21.58814487.06 17.32 497.53 -4.93 487.06196,17.31758508.20 13.40 519.73 -2.12 508.20238,13.4029526.72 9.72 538.71 -0.43 526.71962,9.72356542.56 6.32 553.96 0.31 542.56202,6.31974555.63 3.44 565.08 0.37 555.62626,3.444565.55 1.41 571.77 0.14 565.55072,1.4063571.84 0.31 573.94 -0.06 571.83602,0.30996573.94 0.06 574.00 0.00 573.9426,0.0574

R = 3.172 c = 0.543 S17Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.20 1.49 0.76 -2.70 0.20091,1.493253.12 6.33 5.07 -6.91 3.12225,6.331388.83 11.58 12.60 -11.74 8.82918,11.58219

17.15 17.03 22.93 -17.07 17.14794,17.0284827.95 22.50 35.72 -22.80 27.94821,22.4964941.09 27.87 50.63 -28.78 41.09424,27.8667656.42 33.03 67.32 -34.80 56.4177,33.0252673.74 37.86 85.53 -40.55 73.7394,37.8579692.87 42.28 105.14 -45.87 92.86929,42.27798

113.60 46.18 125.84 -50.64 113.5956,46.18215135.68 49.48 147.31 -54.63 135.67941,49.48359158.88 52.10 169.35 -57.50 158.87637,52.09542182.93 53.94 191.83 -59.00 182.93127,53.93619207.55 54.89 214.71 -58.87 207.55089,54.89187232.45 54.85 238.01 -56.93 232.45287,54.84843257.30 53.45 261.91 -52.98 257.29512,53.44749282.39 50.16 286.90 -47.22 282.38715,50.15691308.43 45.37 313.11 -40.41 308.42943,45.37308335.29 40.07 340.18 -33.19 335.28621,40.06797362.28 34.77 367.67 -26.02 362.27874,34.76829388.82 29.66 395.04 -19.32 388.82058,29.65866414.39 24.86 421.74 -13.39 414.38502,24.85854438.51 20.42 447.15 -8.47 438.50508,20.42223460.76 16.38 470.66 -4.66 460.75722,16.38231480.76 12.68 491.66 -2.01 480.75591,12.67905498.27 9.20 509.62 -0.41 498.27309,9.19842

Page 9: NREL Phase VI - Test Blade & Aerofoil Geometry

513.26 5.98 524.04 0.29 513.25989,5.97843525.62 3.26 534.56 0.35 525.61857,3.258535.01 1.33 540.89 0.13 535.00704,1.33035540.95 0.29 542.95 -0.05 540.95289,0.29322542.95 0.05 543.00 0.00 542.9457,0.0543

R = 3.185 c = 0.542 S18Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.20 1.49 0.76 -2.70 0.20054,1.49053.12 6.32 5.06 -6.89 3.1165,6.319728.81 11.56 12.58 -11.72 8.81292,11.56086

17.12 17.00 22.89 -17.04 17.11636,16.9971227.90 22.46 35.66 -22.76 27.89674,22.4550641.02 27.82 50.54 -28.73 41.01856,27.8154456.31 32.96 67.19 -34.73 56.3138,32.9644473.60 37.79 85.38 -40.47 73.6036,37.7882492.70 42.20 104.94 -45.78 92.69826,42.20012

113.39 46.10 125.61 -50.55 113.3864,46.0971135.43 49.39 147.04 -54.53 135.42954,49.39246158.58 52.00 169.04 -57.39 158.58378,51.99948182.59 53.84 191.48 -58.89 182.59438,53.83686207.17 54.79 214.31 -58.76 207.16866,54.79078232.02 54.75 237.57 -56.82 232.02478,54.74742256.82 53.35 261.43 -52.88 256.82128,53.34906281.87 50.06 286.38 -47.14 281.8671,50.06454307.86 45.29 312.53 -40.34 307.86142,45.28952334.67 39.99 339.56 -33.13 334.66874,39.99418361.61 34.70 366.99 -25.97 361.61156,34.70426388.10 29.60 394.32 -19.28 388.10452,29.60404413.62 24.81 420.96 -13.37 413.62188,24.81276437.70 20.38 446.33 -8.45 437.69752,20.38462459.91 16.35 469.79 -4.66 459.90868,16.35214479.87 12.66 490.75 -2.01 479.87054,12.6557497.36 9.18 508.68 -0.41 497.35546,9.18148512.31 5.97 523.08 0.29 512.31466,5.96742524.65 3.25 533.58 0.35 524.65058,3.252534.02 1.33 539.90 0.13 534.02176,1.3279539.96 0.29 541.95 -0.05 539.95666,0.29268541.95 0.05 542.00 0.00 541.9458,0.0542

R = 3.476 c = 0.512 S19Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.19 1.41 0.72 -2.55 0.18944,1.4082.94 5.97 4.78 -6.51 2.944,5.969928.33 10.92 11.88 -11.07 8.32512,10.92096

16.17 16.06 21.62 -16.10 16.16896,16.0563226.35 21.21 33.68 -21.50 26.35264,21.2121638.75 26.28 47.74 -27.14 38.74816,26.2758453.20 31.14 63.47 -32.81 53.1968,31.1398469.53 35.70 80.65 -38.23 69.5296,35.6966487.57 39.86 99.13 -43.25 87.56736,39.86432

107.11 43.55 118.66 -47.75 107.1104,43.5456

Page 10: NREL Phase VI - Test Blade & Aerofoil Geometry

127.93 46.66 138.90 -51.51 127.93344,46.65856149.81 49.12 159.68 -54.22 149.80608,49.12128172.49 50.86 180.88 -55.63 172.48768,50.85696195.70 51.76 202.45 -55.51 195.70176,51.75808219.18 51.72 224.42 -53.68 219.18208,51.71712242.61 50.40 246.96 -49.95 242.60608,50.39616266.27 47.29 270.53 -44.53 266.2656,47.29344290.82 42.78 295.23 -38.10 290.82112,42.78272316.14 37.78 320.76 -31.29 316.14464,37.78048341.60 32.78 346.68 -24.54 341.59616,32.78336366.62 27.97 372.49 -18.22 366.62272,27.96544390.73 23.44 397.66 -12.63 390.72768,23.43936413.47 19.26 421.62 -7.98 413.47072,19.25632434.45 15.45 443.79 -4.40 434.45248,15.44704453.31 11.96 463.59 -1.89 453.30944,11.9552469.83 8.67 480.52 -0.38 469.82656,8.67328483.96 5.64 494.13 0.28 483.95776,5.63712495.61 3.07 504.04 0.33 495.61088,3.072504.46 1.25 510.01 0.12 504.46336,1.2544510.07 0.28 511.95 -0.05 510.06976,0.27648511.95 0.05 512.00 0.00 511.9488,0.0512

R = 3.781 c = 0.482 S20Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.18 1.33 0.67 -2.40 0.17834,1.32552.77 5.62 4.50 -6.13 2.7715,5.620127.84 10.28 11.19 -10.42 7.83732,10.28106

15.22 15.12 20.35 -15.15 15.22156,15.1155224.81 19.97 31.71 -20.24 24.80854,19.9692636.48 24.74 44.95 -25.55 36.47776,24.7362450.08 29.32 59.75 -30.89 50.0798,29.3152465.46 33.61 75.92 -35.99 65.4556,33.6050482.44 37.53 93.32 -40.71 82.43646,37.52852

100.83 40.99 111.70 -44.95 100.8344,40.9941120.44 43.92 130.76 -48.49 120.43734,43.92466141.03 46.24 150.33 -51.04 141.02838,46.24308162.38 47.88 170.28 -52.37 162.38098,47.87706184.23 48.73 190.59 -52.26 184.23486,48.72538206.34 48.69 211.27 -50.53 206.33938,48.68682228.39 47.44 232.49 -47.02 228.39088,47.44326250.66 44.52 254.67 -41.92 250.6641,44.52234273.78 40.28 277.94 -35.87 273.78082,40.27592297.62 35.57 301.97 -29.46 297.62054,35.56678321.58 30.86 326.36 -23.10 321.58076,30.86246345.14 26.33 350.66 -17.15 345.14092,26.32684367.83 22.07 374.36 -11.89 367.83348,22.06596389.24 18.13 396.92 -7.51 389.24392,18.12802409.00 14.54 417.78 -4.14 408.99628,14.54194426.75 11.25 436.43 -1.78 426.74834,11.2547442.30 8.17 452.37 -0.36 442.29766,8.16508455.60 5.31 465.17 0.26 455.60086,5.30682466.57 2.89 474.51 0.31 466.57118,2.892474.90 1.18 480.13 0.12 474.90496,1.1809

Page 11: NREL Phase VI - Test Blade & Aerofoil Geometry

480.18 0.26 481.95 -0.05 480.18286,0.26028481.95 0.05 482.00 0.00 481.9518,0.0482

R = 4.023 c = 0.457 S21Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.17 1.26 0.64 -2.28 0.16909,1.256752.63 5.33 4.26 -5.81 2.62775,5.328627.43 9.75 10.61 -9.88 7.43082,9.74781

14.43 14.33 19.30 -14.37 14.43206,14.3315223.52 18.93 30.07 -19.19 23.52179,18.9335134.59 23.45 42.62 -24.23 34.58576,23.4532447.48 27.79 56.65 -29.28 47.4823,27.7947462.06 31.86 71.99 -34.12 62.0606,31.8620478.16 35.58 88.48 -38.60 78.16071,35.5820295.60 38.87 105.91 -42.62 95.6044,38.86785

114.19 41.65 123.98 -45.97 114.19059,41.64641133.71 43.84 142.53 -48.39 133.71363,43.84458153.96 45.39 161.45 -49.66 153.95873,45.39381174.68 46.20 180.70 -49.55 174.67911,46.19813195.64 46.16 200.31 -47.91 195.63713,46.16157216.54 44.98 220.43 -44.58 216.54488,44.98251237.66 42.21 241.47 -39.75 237.66285,42.21309259.58 38.19 263.52 -34.01 259.58057,38.18692282.18 33.72 286.31 -27.93 282.18379,33.72203304.90 29.26 309.43 -21.90 304.90126,29.26171327.24 24.96 332.48 -16.26 327.23942,24.96134348.75 20.92 354.94 -11.27 348.75498,20.92146369.05 17.19 376.33 -7.12 369.05492,17.18777387.78 13.79 396.11 -3.93 387.78278,13.78769404.61 10.67 413.79 -1.69 404.61409,10.67095419.36 7.74 428.90 -0.34 419.35691,7.74158431.97 5.03 441.05 0.25 431.97011,5.03157442.37 2.74 449.90 0.30 442.37143,2.742450.27 1.12 455.23 0.11 450.27296,1.11965455.28 0.25 456.95 -0.05 455.27711,0.24678456.95 0.05 457.00 0.00 456.9543,0.0457

R = 4.086 c = 0.451 S22Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.17 1.24 0.63 -2.25 0.16687,1.240252.59 5.26 4.21 -5.74 2.59325,5.258667.33 9.62 10.47 -9.75 7.33326,9.61983

14.24 14.14 19.05 -14.18 14.24258,14.1433623.21 18.68 29.67 -18.94 23.21297,18.6849334.13 23.15 42.06 -23.91 34.13168,23.1453246.86 27.43 55.91 -28.90 46.8589,27.4298261.25 31.44 71.04 -33.68 61.2458,31.4437277.13 35.11 87.32 -38.10 77.13453,35.1148694.35 38.36 104.52 -42.06 94.3492,38.35755

112.69 41.10 122.35 -45.37 112.69137,41.09963131.96 43.27 140.66 -47.76 131.95809,43.26894151.94 44.80 159.33 -49.01 151.93739,44.79783

Page 12: NREL Phase VI - Test Blade & Aerofoil Geometry

172.39 45.59 178.33 -48.90 172.38573,45.59159193.07 45.56 197.68 -47.28 193.06859,45.55551213.70 44.39 217.54 -44.00 213.70184,44.39193234.54 41.66 238.29 -39.22 234.54255,41.65887256.17 37.69 260.06 -33.56 256.17251,37.68556278.48 33.28 282.55 -27.57 278.47897,33.27929300.90 28.88 305.37 -21.61 300.89818,28.87753322.94 24.63 328.11 -16.05 322.94306,24.63362344.18 20.65 350.28 -11.12 344.17614,20.64678364.21 16.96 371.39 -7.03 364.20956,16.96211382.69 13.61 390.91 -3.87 382.69154,13.60667399.30 10.53 408.36 -1.67 399.30187,10.53085413.85 7.64 423.27 -0.34 413.85113,7.63994426.30 4.97 435.26 0.24 426.29873,4.96551436.56 2.71 443.99 0.29 436.56349,2.706444.36 1.10 449.25 0.11 444.36128,1.10495449.30 0.24 450.95 -0.05 449.29973,0.24354450.95 0.05 451.00 0.00 450.9549,0.0451

R = 4.391 c = 0.420 S23Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.16 1.16 0.59 -2.09 0.1554,1.1552.42 4.90 3.92 -5.34 2.415,4.89726.83 8.96 9.75 -9.08 6.8292,8.9586

13.26 13.17 17.74 -13.20 13.2636,13.171221.62 17.40 27.63 -17.64 21.6174,17.400631.79 21.55 39.17 -22.26 31.7856,21.554443.64 25.54 52.07 -26.91 43.638,25.544457.04 29.28 66.16 -31.36 57.036,29.282471.83 32.70 81.32 -35.48 71.8326,32.701287.86 35.72 97.34 -39.17 87.864,35.721

104.95 38.27 113.94 -42.25 104.9454,38.2746122.89 40.29 130.99 -44.47 122.8878,40.2948141.49 41.72 148.38 -45.64 141.4938,41.7186160.54 42.46 166.07 -45.54 160.5366,42.4578179.80 42.42 184.09 -44.03 179.7978,42.4242199.01 41.34 202.58 -40.98 199.0128,41.3406218.42 38.80 221.92 -36.53 218.421,38.7954238.56 35.10 242.18 -31.26 238.5642,35.0952259.34 30.99 263.13 -25.67 259.3374,30.9918280.22 26.89 284.38 -20.13 280.2156,26.8926300.75 22.94 305.56 -14.94 300.7452,22.9404320.52 19.23 326.21 -10.36 320.5188,19.2276339.18 15.80 345.86 -6.55 339.1752,15.7962356.39 12.67 364.04 -3.61 356.3868,12.6714371.86 9.81 380.29 -1.55 371.8554,9.807385.40 7.11 394.18 -0.32 385.4046,7.1148397.00 4.62 405.34 0.23 396.9966,4.6242406.56 2.52 413.47 0.27 406.5558,2.52413.82 1.03 418.37 0.10 413.8176,1.029418.42 0.23 419.96 -0.04 418.4166,0.2268419.96 0.04 420.00 0.00 419.958,0.042

Page 13: NREL Phase VI - Test Blade & Aerofoil Geometry

R = 4.696 c = 0.389 S24Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.14 1.07 0.54 -1.94 0.14393,1.069752.24 4.54 3.63 -4.95 2.23675,4.535746.33 8.30 9.03 -8.41 6.32514,8.29737

12.28 12.20 16.43 -12.23 12.28462,12.1990420.02 16.12 25.59 -16.33 20.02183,16.1162729.44 19.96 36.27 -20.62 29.43952,19.9634840.42 23.66 48.22 -24.93 40.4171,23.6589852.83 27.12 61.28 -29.05 52.8262,27.1210866.53 30.29 75.32 -32.86 66.53067,30.2875481.38 33.08 90.15 -36.28 81.3788,33.0844597.20 35.45 105.53 -39.13 97.19943,35.44957

113.82 37.32 121.32 -41.19 113.81751,37.32066131.05 38.64 137.43 -42.27 131.05021,38.63937148.69 39.32 153.81 -42.18 148.68747,39.32401166.53 39.29 170.51 -40.78 166.52701,39.29289184.32 38.29 187.63 -37.95 184.32376,38.28927202.30 35.93 205.54 -33.83 202.29945,35.93193220.96 32.50 224.31 -28.95 220.95589,32.50484240.20 28.70 243.70 -23.78 240.19583,28.70431259.53 24.91 263.39 -18.64 259.53302,24.90767278.55 21.25 283.01 -13.84 278.54734,21.24718296.86 17.81 302.13 -9.59 296.86146,17.80842314.14 14.63 320.33 -6.06 314.14084,14.63029330.08 11.74 337.17 -3.34 330.08206,11.73613344.41 9.08 352.22 -1.44 344.40893,9.08315356.96 6.59 365.08 -0.29 356.95807,6.58966367.69 4.28 375.42 0.21 367.69447,4.28289376.55 2.33 382.95 0.25 376.54811,2.334383.27 0.95 387.49 0.09 383.27392,0.95305387.53 0.21 388.96 -0.04 387.53347,0.21006388.96 0.04 389.00 0.00 388.9611,0.0389

R = 4.780 c = 0.381 S25Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.14 1.05 0.53 -1.90 0.14097,1.047752.19 4.44 3.55 -4.85 2.19075,4.442466.20 8.13 8.84 -8.24 6.19506,8.12673

12.03 11.95 16.09 -11.98 12.03198,11.9481619.61 15.78 25.07 -16.00 19.61007,15.7848328.83 19.55 35.53 -20.20 28.83408,19.5529239.59 23.17 47.23 -24.41 39.5859,23.1724251.74 26.56 60.02 -28.45 51.7398,26.5633265.16 29.66 73.77 -32.18 65.16243,29.6646679.71 32.40 88.30 -35.53 79.7052,32.4040595.20 34.72 103.36 -38.33 95.20047,34.72053

111.48 36.55 118.83 -40.34 111.47679,36.55314128.36 37.84 134.60 -41.40 128.35509,37.84473145.63 38.52 150.65 -41.31 145.62963,38.51529163.10 38.48 167.00 -39.94 163.10229,38.48481180.53 37.50 183.77 -37.17 180.53304,37.50183

Page 14: NREL Phase VI - Test Blade & Aerofoil Geometry

198.14 35.19 201.31 -33.14 198.13905,35.19297216.41 31.84 219.70 -28.35 216.41181,31.83636235.26 28.11 238.69 -23.29 235.25607,28.11399254.20 24.40 257.98 -18.26 254.19558,24.39543272.82 20.81 277.19 -13.56 272.81886,20.81022290.76 17.44 295.92 -9.40 290.75634,17.44218307.68 14.33 313.75 -5.94 307.68036,14.32941323.29 11.49 330.24 -3.27 323.29374,11.49477337.33 8.90 344.98 -1.41 337.32597,8.89635349.62 6.45 357.58 -0.29 349.61703,6.45414360.13 4.19 367.70 0.21 360.13263,4.19481368.80 2.29 375.08 0.25 368.80419,2.286375.39 0.93 379.52 0.09 375.39168,0.93345379.56 0.21 380.96 -0.04 379.56363,0.20574380.96 0.04 381.00 0.00 380.9619,0.0381

R = 5.000 c = 0.358 S26Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.13 0.98 0.50 -1.78 0.13246,0.98452.06 4.17 3.34 -4.55 2.0585,4.174285.82 7.64 8.31 -7.74 5.82108,7.63614

11.31 11.23 15.12 -11.26 11.30564,11.2268818.43 14.83 23.55 -15.03 18.42626,14.8319427.09 18.37 33.38 -18.98 27.09344,18.3725637.20 21.77 44.38 -22.94 37.1962,21.7735648.62 24.96 56.39 -26.73 48.6164,24.9597661.23 27.87 69.32 -30.24 61.22874,27.8738874.89 30.45 82.97 -33.39 74.8936,30.447989.45 32.62 97.12 -36.01 89.45346,32.62454

104.75 34.35 111.65 -37.91 104.74722,34.34652120.61 35.56 126.47 -38.90 120.60662,35.56014136.84 36.19 141.56 -38.81 136.83834,36.19022153.26 36.16 156.92 -37.53 153.25622,36.16158169.63 35.24 172.68 -34.93 169.63472,35.23794186.18 33.07 189.16 -31.14 186.1779,33.06846203.35 29.91 206.43 -26.64 203.34758,29.91448221.05 26.42 224.28 -21.88 221.05426,26.41682238.85 22.92 242.40 -17.16 238.85044,22.92274256.35 19.55 260.45 -12.74 256.34948,19.55396273.20 16.39 278.05 -8.83 273.20412,16.38924289.11 13.46 294.81 -5.58 289.10648,13.46438303.78 10.80 310.30 -3.08 303.77732,10.80086316.96 8.36 324.15 -1.32 316.96246,8.3593328.51 6.06 335.99 -0.27 328.51154,6.06452338.39 3.94 345.50 0.19 338.39234,3.94158346.54 2.15 352.44 0.23 346.54042,2.148352.73 0.88 356.61 0.09 352.73024,0.8771356.65 0.19 357.93 -0.04 356.65034,0.19332357.93 0.04 358.00 0.00 357.9284,0.0358

R = 5.000 c = 0.358 S26Upper Surface Lower Surface Upper Surface

X Y X Y 0,0

Page 15: NREL Phase VI - Test Blade & Aerofoil Geometry

0.13 0.98 0.50 -1.78 0.13246,0.98452.06 4.17 3.34 -4.55 2.0585,4.174285.82 7.64 8.31 -7.74 5.82108,7.63614

11.31 11.23 15.12 -11.26 11.30564,11.2268818.43 14.83 23.55 -15.03 18.42626,14.8319427.09 18.37 33.38 -18.98 27.09344,18.3725637.20 21.77 44.38 -22.94 37.1962,21.7735648.62 24.96 56.39 -26.73 48.6164,24.9597661.23 27.87 69.32 -30.24 61.22874,27.8738874.89 30.45 82.97 -33.39 74.8936,30.447989.45 32.62 97.12 -36.01 89.45346,32.62454

104.75 34.35 111.65 -37.91 104.74722,34.34652120.61 35.56 126.47 -38.90 120.60662,35.56014136.84 36.19 141.56 -38.81 136.83834,36.19022153.26 36.16 156.92 -37.53 153.25622,36.16158169.63 35.24 172.68 -34.93 169.63472,35.23794186.18 33.07 189.16 -31.14 186.1779,33.06846203.35 29.91 206.43 -26.64 203.34758,29.91448221.05 26.42 224.28 -21.88 221.05426,26.41682238.85 22.92 242.40 -17.16 238.85044,22.92274256.35 19.55 260.45 -12.74 256.34948,19.55396273.20 16.39 278.05 -8.83 273.20412,16.38924289.11 13.46 294.81 -5.58 289.10648,13.46438303.78 10.80 310.30 -3.08 303.77732,10.80086316.96 8.36 324.15 -1.32 316.96246,8.3593328.51 6.06 335.99 -0.27 328.51154,6.06452338.39 3.94 345.50 0.19 338.39234,3.94158346.54 2.15 352.44 0.23 346.54042,2.148352.73 0.88 356.61 0.09 352.73024,0.8771356.65 0.19 357.96 -0.04 356.65034,0.19332357.96 0.04 358.00 0.00 357.9642,0.0358

R = 5.305 c = 0.328 S27Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.12 0.90 0.46 -1.63 0.12136,0.9021.89 3.82 3.06 -4.17 1.886,3.824485.33 7.00 7.61 -7.09 5.33328,6.99624

10.36 10.29 13.85 -10.31 10.35824,10.2860816.88 13.59 21.58 -13.77 16.88216,13.5890424.82 16.83 30.59 -17.39 24.82304,16.8329634.08 19.95 40.66 -21.02 34.0792,19.9489644.54 22.87 51.67 -24.49 44.5424,22.8681656.10 25.54 63.51 -27.71 56.09784,25.5380868.62 27.90 76.01 -30.59 68.6176,27.896481.96 29.89 88.98 -33.00 81.95736,29.8906495.97 31.47 102.30 -34.73 95.96952,31.46832

110.50 32.58 115.88 -35.64 110.49992,32.58024125.37 33.16 129.69 -35.56 125.37144,33.15752140.41 33.13 143.77 -34.39 140.41352,33.13128155.42 32.29 158.21 -32.00 155.41952,32.28504170.58 30.30 173.31 -28.53 170.5764,30.29736186.31 27.41 189.13 -24.41 186.30728,27.40768202.53 24.20 205.49 -20.05 202.53016,24.20312

Page 16: NREL Phase VI - Test Blade & Aerofoil Geometry

218.84 21.00 222.09 -15.72 218.83504,21.00184234.87 17.92 238.63 -11.67 234.86768,17.91536250.31 15.02 254.75 -8.09 250.30992,15.01584264.88 12.34 270.10 -5.11 264.87968,12.33608278.32 9.90 284.30 -2.82 278.32112,9.89576290.40 7.66 296.99 -1.21 290.40136,7.6588300.98 5.56 307.83 -0.25 300.98264,5.55632310.04 3.61 316.55 0.18 310.03544,3.61128317.50 1.97 322.90 0.21 317.50072,1.968323.17 0.80 326.73 0.08 323.17184,0.8036326.76 0.18 327.97 -0.03 326.76344,0.17712327.97 0.03 328.00 0.00 327.9672,0.0328

R = 5.532 c = 0.305 S28Upper Surface Lower Surface Upper Surface

X Y X Y 0,00.11 0.84 0.43 -1.52 0.11285,0.838751.75 3.56 2.85 -3.88 1.75375,3.55634.96 6.51 7.08 -6.59 4.9593,6.505659.63 9.56 12.88 -9.59 9.6319,9.5648

15.70 12.64 20.07 -12.81 15.69835,12.6361523.08 15.65 28.44 -16.17 23.0824,15.652631.69 18.55 37.81 -19.54 31.6895,18.550141.42 21.26 48.04 -22.77 41.419,21.264652.16 23.75 59.05 -25.76 52.16415,23.747363.81 25.94 70.68 -28.44 63.806,25.9402576.21 27.79 82.74 -30.68 76.21035,27.7946589.24 29.26 95.12 -32.30 89.23995,29.2617

102.75 30.30 107.75 -33.14 102.75145,30.29565116.58 30.83 120.60 -33.07 116.58015,30.83245130.57 30.81 133.69 -31.98 130.56745,30.80805144.52 30.02 147.11 -29.76 144.5212,30.02115158.62 28.17 161.15 -26.53 158.61525,28.17285173.24 25.49 175.87 -22.70 173.24305,25.4858188.33 22.51 191.08 -18.64 188.32835,22.50595203.49 19.53 206.52 -14.62 203.4899,19.52915218.40 16.66 221.89 -10.85 218.3983,16.6591232.76 13.96 236.89 -7.52 232.7577,13.9629246.31 11.47 251.16 -4.75 246.3058,11.47105258.80 9.20 264.36 -2.62 258.8047,9.20185270.04 7.12 276.16 -1.13 270.03785,7.12175279.88 5.17 286.25 -0.23 279.87715,5.1667288.30 3.36 294.35 0.16 288.29515,3.35805295.24 1.83 300.26 0.20 295.23695,1.83300.51 0.75 303.82 0.07 300.5104,0.74725303.85 0.16 304.97 -0.03 303.85015,0.1647304.97 0.03 305.00 0.00 304.9695,0.0305

Page 17: NREL Phase VI - Test Blade & Aerofoil Geometry

Lower Surface0 737,0

1.0318,-3.67026 1 736.96315,-0.036856.87621,-9.37464 2 734.14044,0.17688

17.10577,-15.93394 3 725.54702,0.4790531.12351,-23.17128 4 711.27133,0.3979848.48723,-30.94663 5 691.68924,-0.5527568.72525,-39.06837 6 667.31665,-2.726991.36589,-47.22696 7 638.80949,-6.33083

116.09224,-55.03179 8 606.90476,-11.48983142.69794,-62.25439 9 572.41316,-18.17442170.79975,-68.73262 10 536.18224,-26.22246199.94073,-74.1422 11 499.0227,-35.31704

229.85556,-78.04093 12 461.72313,-45.04544260.36736,-80.08242 13 424.97631,-54.84754291.41717,-79.90554 14 389.40869,-64.09689323.04184,-77.26708 15 355.48458,-71.90172355.48458,-71.90172 16 323.04184,-77.26708389.40869,-64.09689 17 291.41717,-79.90554

0.00 0.05 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.00

-0.15

-0.10

-0.05

0.00

0.05

0.10

0.15

Page 18: NREL Phase VI - Test Blade & Aerofoil Geometry

424.97631,-54.84754 18 260.36736,-80.08242461.72313,-45.04544 19 229.85556,-78.04093499.0227,-35.31704 20 199.94073,-74.1422

536.18224,-26.22246 21 170.79975,-68.73262572.41316,-18.17442 22 142.69794,-62.25439606.90476,-11.48983 23 116.09224,-55.03179638.80949,-6.33083 24 91.36589,-47.22696667.31665,-2.7269 25 68.72525,-39.06837

691.68924,-0.55275 26 48.48723,-30.94663711.27133,0.39798 27 31.12351,-23.17128725.54702,0.47905 28 17.10577,-15.93394734.14044,0.17688 29 6.87621,-9.37464736.8526,-0.1474 30 1.0318,-3.67026

737,0 31

Lower Surface0

1.0192,-3.62544 1 728,06.79224,-9.26016 2 727.9636,-0.0364

16.89688,-15.73936 3 725.17536,0.1747230.74344,-22.88832 4 716.68688,0.473247.89512,-30.56872 5 702.58552,0.39312

67.886,-38.59128 6 683.24256,-0.54690.25016,-46.65024 7 659.1676,-2.6936

114.67456,-54.35976 8 631.00856,-6.25352140.95536,-61.49416 9 599.49344,-11.34952

168.714,-67.89328 10 565.42304,-17.95248197.49912,-73.2368 11 529.63456,-25.90224

227.04864,-77.08792 12 492.9288,-34.88576257.18784,-79.10448 13 456.08472,-44.49536287.85848,-78.92976 14 419.78664,-54.17776319.09696,-76.32352 15 384.65336,-63.31416351.14352,-71.02368 16 351.14352,-71.02368384.65336,-63.31416 17 319.09696,-76.32352419.78664,-54.17776 18 287.85848,-78.92976456.08472,-44.49536 19 257.18784,-79.10448492.9288,-34.88576 20 227.04864,-77.08792

529.63456,-25.90224 21 197.49912,-73.2368565.42304,-17.95248 22 168.714,-67.89328599.49344,-11.34952 23 140.95536,-61.49416631.00856,-6.25352 24 114.67456,-54.35976

659.1676,-2.6936 25 90.25016,-46.65024683.24256,-0.546 26 67.886,-38.59128

702.58552,0.39312 27 47.89512,-30.56872716.68688,0.4732 28 30.74344,-22.88832

725.17536,0.17472 29 16.89688,-15.73936727.9272,-0.0728 30 6.79224,-9.26016

728,0 31 1.0192,-3.62544

Lower Surface Lower Surface0

0.9954,-3.54078 1 711,0

Page 19: NREL Phase VI - Test Blade & Aerofoil Geometry

6.63363,-9.04392 2 710.96445,-0.0355516.50231,-15.37182 3 708.24132,0.1706430.02553,-22.35384 4 699.95106,0.4621546.77669,-29.85489 5 686.17899,0.3839466.30075,-37.69011 6 667.28772,-0.5332588.14267,-45.56088 7 643.77495,-2.6307

111.99672,-53.09037 8 616.27347,-6.10749137.66382,-60.05817 9 585.49428,-11.08449164.77425,-66.30786 10 552.21948,-17.53326192.88719,-71.5266 11 517.26672,-25.29738

221.74668,-75.28779 12 481.4181,-34.07112251.18208,-77.25726 13 445.43439,-43.45632281.13651,-77.08662 14 409.98393,-52.91262311.64552,-74.54124 15 375.67107,-61.83567342.94374,-69.36516 16 342.94374,-69.36516375.67107,-61.83567 17 311.64552,-74.54124409.98393,-52.91262 18 281.13651,-77.08662445.43439,-43.45632 19 251.18208,-77.25726481.4181,-34.07112 20 221.74668,-75.28779

517.26672,-25.29738 21 192.88719,-71.5266552.21948,-17.53326 22 164.77425,-66.30786585.49428,-11.08449 23 137.66382,-60.05817616.27347,-6.10749 24 111.99672,-53.09037643.77495,-2.6307 25 88.14267,-45.56088

667.28772,-0.53325 26 66.30075,-37.69011686.17899,0.38394 27 46.77669,-29.85489699.95106,0.46215 28 30.02553,-22.35384708.24132,0.17064 29 16.50231,-15.37182710.9289,-0.0711 30 6.63363,-9.04392

711,0 31 0.9954,-3.54078

Lower Surface Lower Surface0

0.9758,-3.47106 1 697,06.50301,-8.86584 2 696.96515,-0.03485

16.17737,-15.06914 3 694.29564,0.1672829.43431,-21.91368 4 686.16862,0.4530545.85563,-29.26703 5 672.66773,0.3763864.99525,-36.94797 6 654.14844,-0.5227586.40709,-44.66376 7 631.09865,-2.5789

109.79144,-52.04499 8 604.13869,-5.98723134.95314,-58.87559 9 573.96556,-10.86623161.52975,-65.00222 10 541.34596,-17.18802189.08913,-70.1182 11 507.08144,-24.79926

217.38036,-73.80533 12 471.9387,-33.40024246.23616,-75.73602 13 436.66353,-42.60064275.60077,-75.56874 14 401.91111,-51.87074305.50904,-73.07348 15 368.27389,-60.61809336.19098,-67.99932 16 336.19098,-67.99932368.27389,-60.61809 17 305.50904,-73.07348401.91111,-51.87074 18 275.60077,-75.56874436.66353,-42.60064 19 246.23616,-75.73602471.9387,-33.40024 20 217.38036,-73.80533

Page 20: NREL Phase VI - Test Blade & Aerofoil Geometry

507.08144,-24.79926 21 189.08913,-70.1182541.34596,-17.18802 22 161.52975,-65.00222573.96556,-10.86623 23 134.95314,-58.87559604.13869,-5.98723 24 109.79144,-52.04499631.09865,-2.5789 25 86.40709,-44.66376

654.14844,-0.52275 26 64.99525,-36.94797672.66773,0.37638 27 45.85563,-29.26703686.16862,0.45305 28 29.43431,-21.91368694.29564,0.16728 29 16.17737,-15.06914696.9303,-0.0697 30 6.50301,-8.86584

697,0 31 0.9758,-3.47106

Lower Surface Lower Surface0

0.9324,-3.31668 1 666,06.21378,-8.47152 2 665.9667,-0.0333

15.45786,-14.39892 3 663.41592,0.1598428.12518,-20.93904 4 655.65036,0.432943.81614,-27.96534 5 642.74994,0.3596462.1045,-35.30466 6 625.05432,-0.4995

82.56402,-42.67728 7 603.0297,-2.4642104.90832,-49.73022 8 577.26882,-5.72094128.95092,-56.25702 9 548.43768,-10.38294154.3455,-62.11116 10 517.26888,-16.42356180.67914,-66.9996 11 484.52832,-23.69628

207.71208,-70.52274 12 450.9486,-31.91472235.28448,-72.36756 13 417.24234,-40.70592263.34306,-72.20772 14 384.03558,-49.56372291.92112,-69.82344 15 351.89442,-57.92202321.23844,-64.97496 16 321.23844,-64.97496351.89442,-57.92202 17 291.92112,-69.82344384.03558,-49.56372 18 263.34306,-72.20772417.24234,-40.70592 19 235.28448,-72.36756450.9486,-31.91472 20 207.71208,-70.52274

484.52832,-23.69628 21 180.67914,-66.9996517.26888,-16.42356 22 154.3455,-62.11116548.43768,-10.38294 23 128.95092,-56.25702577.26882,-5.72094 24 104.90832,-49.73022

603.0297,-2.4642 25 82.56402,-42.67728625.05432,-0.4995 26 62.1045,-35.30466642.74994,0.35964 27 43.81614,-27.96534655.65036,0.4329 28 28.12518,-20.93904

663.41592,0.15984 29 15.45786,-14.39892665.9334,-0.0666 30 6.21378,-8.47152

666,0 31 0.9324,-3.31668

Lower Surface Lower Surface0

0.8904,-3.16728 1 636,05.93388,-8.08992 2 635.9682,-0.0318

14.76156,-13.75032 3 633.53232,0.1526426.85828,-19.99584 4 626.11656,0.4134

Page 21: NREL Phase VI - Test Blade & Aerofoil Geometry

41.84244,-26.70564 5 613.79724,0.3434459.307,-33.71436 6 596.89872,-0.477

78.84492,-40.75488 7 575.8662,-2.3532100.18272,-47.49012 8 551.26572,-5.46324123.14232,-53.72292 9 523.73328,-9.91524

147.393,-59.31336 10 493.96848,-15.68376172.54044,-63.9816 11 462.70272,-22.62888

198.35568,-67.34604 12 430.6356,-30.47712224.68608,-69.10776 13 398.44764,-38.87232251.48076,-68.95512 14 366.73668,-47.33112278.77152,-66.67824 15 336.04332,-55.31292306.76824,-62.04816 16 306.76824,-62.04816336.04332,-55.31292 17 278.77152,-66.67824366.73668,-47.33112 18 251.48076,-68.95512398.44764,-38.87232 19 224.68608,-69.10776430.6356,-30.47712 20 198.35568,-67.34604

462.70272,-22.62888 21 172.54044,-63.9816493.96848,-15.68376 22 147.393,-59.31336523.73328,-9.91524 23 123.14232,-53.72292551.26572,-5.46324 24 100.18272,-47.49012

575.8662,-2.3532 25 78.84492,-40.75488596.89872,-0.477 26 59.307,-33.71436

613.79724,0.34344 27 41.84244,-26.70564626.11656,0.4134 28 26.85828,-19.99584

633.53232,0.15264 29 14.76156,-13.75032635.9364,-0.0636 30 5.93388,-8.08992

636,0 31 0.8904,-3.16728

Lower Surface Lower Surface0

0.8778,-3.12246 1 627,05.84991,-7.97544 2 626.96865,-0.03135

14.55267,-13.55574 3 624.56724,0.1504826.47821,-19.71288 4 617.25642,0.4075541.25033,-26.32773 5 605.11143,0.3385858.46775,-33.23727 6 588.45204,-0.4702577.72919,-40.17816 7 567.71715,-2.319998.76504,-46.81809 8 543.46479,-5.38593

121.39974,-52.96269 9 516.32196,-9.77493145.30725,-58.47402 10 486.97836,-15.46182170.09883,-63.0762 11 456.15504,-22.30866

195.54876,-66.39303 12 424.5417,-30.04584221.50656,-68.12982 13 392.80923,-38.32224247.92207,-67.97934 14 361.54701,-46.66134274.82664,-65.73468 15 331.28799,-54.53019302.42718,-61.17012 16 302.42718,-61.17012331.28799,-54.53019 17 274.82664,-65.73468361.54701,-46.66134 18 247.92207,-67.97934392.80923,-38.32224 19 221.50656,-68.12982424.5417,-30.04584 20 195.54876,-66.39303

456.15504,-22.30866 21 170.09883,-63.0762486.97836,-15.46182 22 145.30725,-58.47402516.32196,-9.77493 23 121.39974,-52.96269

Page 22: NREL Phase VI - Test Blade & Aerofoil Geometry

543.46479,-5.38593 24 98.76504,-46.81809567.71715,-2.3199 25 77.72919,-40.17816

588.45204,-0.47025 26 58.46775,-33.23727605.11143,0.33858 27 41.25033,-26.32773617.25642,0.40755 28 26.47821,-19.71288624.56724,0.15048 29 14.55267,-13.55574626.9373,-0.0627 30 5.84991,-7.97544

627,0 31 0.8778,-3.12246

Lower Surface Lower Surface0

0.847,-3.0129 1 605,05.64465,-7.6956 2 604.96975,-0.03025

14.04205,-13.0801 3 602.6526,0.145225.54915,-19.0212 4 595.5983,0.39325

39.80295,-25.40395 5 583.87945,0.326756.41625,-32.07105 6 567.8046,-0.4537575.00185,-38.7684 7 547.79725,-2.238595.2996,-45.17535 8 524.39585,-5.19695

117.1401,-51.10435 9 498.2054,-9.43195140.20875,-56.4223 10 469.8914,-14.9193164.13045,-60.863 11 440.1496,-21.5259

188.6874,-64.06345 12 409.6455,-28.9916213.7344,-65.7393 13 379.02645,-36.9776

239.22305,-65.5941 14 348.86115,-45.0241265.1836,-63.4282 15 319.66385,-52.61685291.8157,-59.0238 16 291.8157,-59.0238

319.66385,-52.61685 17 265.1836,-63.4282348.86115,-45.0241 18 239.22305,-65.5941379.02645,-36.9776 19 213.7344,-65.7393409.6455,-28.9916 20 188.6874,-64.06345440.1496,-21.5259 21 164.13045,-60.863469.8914,-14.9193 22 140.20875,-56.4223498.2054,-9.43195 23 117.1401,-51.10435

524.39585,-5.19695 24 95.2996,-45.17535547.79725,-2.2385 25 75.00185,-38.7684567.8046,-0.45375 26 56.41625,-32.07105583.87945,0.3267 27 39.80295,-25.40395595.5983,0.39325 28 25.54915,-19.0212602.6526,0.1452 29 14.04205,-13.0801604.9395,-0.0605 30 5.64465,-7.6956

605,0 31 0.847,-3.0129

Lower Surface Lower Surface0

0.8036,-2.85852 1 574,05.35542,-7.30128 2 573.9713,-0.0287

13.32254,-12.40988 3 571.77288,0.1377624.24002,-18.04656 4 565.08004,0.373137.76346,-24.10226 5 553.96166,0.3099653.5255,-30.42774 6 538.71048,-0.4305

71.15878,-36.78192 7 519.7283,-2.1238

Page 23: NREL Phase VI - Test Blade & Aerofoil Geometry

90.41648,-42.86058 8 497.52598,-4.93066111.13788,-48.48578 9 472.67752,-8.94866133.0245,-53.53124 10 445.81432,-14.15484155.72046,-57.7444 11 417.59648,-20.42292

179.01912,-60.78086 12 388.6554,-27.50608202.78272,-62.37084 13 359.60526,-35.08288226.96534,-62.23308 14 330.98562,-42.71708251.59568,-60.17816 15 303.28438,-49.92078276.86316,-55.99944 16 276.86316,-55.99944303.28438,-49.92078 17 251.59568,-60.17816330.98562,-42.71708 18 226.96534,-62.23308359.60526,-35.08288 19 202.78272,-62.37084388.6554,-27.50608 20 179.01912,-60.78086

417.59648,-20.42292 21 155.72046,-57.7444445.81432,-14.15484 22 133.0245,-53.53124472.67752,-8.94866 23 111.13788,-48.48578497.52598,-4.93066 24 90.41648,-42.86058

519.7283,-2.1238 25 71.15878,-36.78192538.71048,-0.4305 26 53.5255,-30.42774553.96166,0.30996 27 37.76346,-24.10226565.08004,0.3731 28 24.24002,-18.04656

571.77288,0.13776 29 13.32254,-12.40988573.9426,-0.0574 30 5.35542,-7.30128

574,0 31 0.8036,-2.85852

Lower Surface Lower Surface0

0.7602,-2.70414 1 543,05.06619,-6.90696 2 542.97285,-0.02715

12.60303,-11.73966 3 540.89316,0.1303222.93089,-17.07192 4 534.56178,0.3529535.72397,-22.80057 5 524.04387,0.2932250.63475,-28.78443 6 509.61636,-0.4072567.31571,-34.79544 7 491.65935,-2.009185.53336,-40.54581 8 470.65611,-4.66437

105.13566,-45.86721 9 447.14964,-8.46537125.84025,-50.64018 10 421.73724,-13.39038147.31047,-54.6258 11 395.04336,-19.31994

169.35084,-57.49827 12 367.6653,-26.02056191.83104,-59.00238 13 340.18407,-33.18816214.70763,-58.87206 14 313.11009,-40.41006238.00776,-56.92812 15 286.90491,-47.22471261.91062,-52.97508 16 261.91062,-52.97508286.90491,-47.22471 17 238.00776,-56.92812313.11009,-40.41006 18 214.70763,-58.87206340.18407,-33.18816 19 191.83104,-59.00238367.6653,-26.02056 20 169.35084,-57.49827

395.04336,-19.31994 21 147.31047,-54.6258421.73724,-13.39038 22 125.84025,-50.64018447.14964,-8.46537 23 105.13566,-45.86721470.65611,-4.66437 24 85.53336,-40.54581491.65935,-2.0091 25 67.31571,-34.79544

509.61636,-0.40725 26 50.63475,-28.78443

Page 24: NREL Phase VI - Test Blade & Aerofoil Geometry

524.04387,0.29322 27 35.72397,-22.80057534.56178,0.35295 28 22.93089,-17.07192540.89316,0.13032 29 12.60303,-11.73966542.9457,-0.0543 30 5.06619,-6.90696

543,0 31 0.7602,-2.70414

Lower Surface Lower Surface0

0.7588,-2.69916 1 542,05.05686,-6.89424 2 541.9729,-0.0271

12.57982,-11.71804 3 539.89704,0.1300822.88866,-17.04048 4 533.57732,0.352335.65818,-22.75858 5 523.07878,0.2926850.5415,-28.73142 6 508.67784,-0.4065

67.19174,-34.73136 7 490.7539,-2.005485.37584,-40.47114 8 469.78934,-4.65578

104.94204,-45.78274 9 446.32616,-8.44978125.6085,-50.54692 10 420.96056,-13.36572147.03918,-54.5252 11 394.31584,-19.28436

169.03896,-57.39238 12 366.9882,-25.97264191.47776,-58.89372 13 339.55758,-33.12704214.31222,-58.76364 14 312.53346,-40.33564237.56944,-56.82328 15 286.37654,-47.13774261.42828,-52.87752 16 261.42828,-52.87752286.37654,-47.13774 17 237.56944,-56.82328312.53346,-40.33564 18 214.31222,-58.76364339.55758,-33.12704 19 191.47776,-58.89372366.9882,-25.97264 20 169.03896,-57.39238

394.31584,-19.28436 21 147.03918,-54.5252420.96056,-13.36572 22 125.6085,-50.54692446.32616,-8.44978 23 104.94204,-45.78274469.78934,-4.65578 24 85.37584,-40.47114

490.7539,-2.0054 25 67.19174,-34.73136508.67784,-0.4065 26 50.5415,-28.73142523.07878,0.29268 27 35.65818,-22.75858533.57732,0.3523 28 22.88866,-17.04048

539.89704,0.13008 29 12.57982,-11.71804541.9458,-0.0542 30 5.05686,-6.89424

542,0 31 0.7588,-2.69916

Lower Surface Lower Surface0

0.7168,-2.54976 1 512,04.77696,-6.51264 2 511.9744,-0.0256

11.88352,-11.06944 3 510.01344,0.1228821.62176,-16.09728 4 504.04352,0.332833.68448,-21.49888 5 494.12608,0.27648

47.744,-27.14112 6 480.52224,-0.38463.47264,-32.80896 7 463.5904,-1.894480.65024,-38.23104 8 443.78624,-4.3980899.13344,-43.24864 9 421.62176,-7.98208118.656,-47.74912 10 397.66016,-12.62592

Page 25: NREL Phase VI - Test Blade & Aerofoil Geometry

138.90048,-51.5072 11 372.49024,-18.21696159.68256,-54.21568 12 346.6752,-24.53504180.87936,-55.63392 13 320.76288,-31.29344202.44992,-55.51104 14 295.23456,-38.10304224.41984,-53.67808 15 270.52544,-44.52864246.95808,-49.95072 16 246.95808,-49.95072270.52544,-44.52864 17 224.41984,-53.67808295.23456,-38.10304 18 202.44992,-55.51104320.76288,-31.29344 19 180.87936,-55.63392346.6752,-24.53504 20 159.68256,-54.21568

372.49024,-18.21696 21 138.90048,-51.5072397.66016,-12.62592 22 118.656,-47.74912421.62176,-7.98208 23 99.13344,-43.24864443.78624,-4.39808 24 80.65024,-38.23104

463.5904,-1.8944 25 63.47264,-32.80896480.52224,-0.384 26 47.744,-27.14112

494.12608,0.27648 27 33.68448,-21.49888504.04352,0.3328 28 21.62176,-16.09728

510.01344,0.12288 29 11.88352,-11.06944511.9488,-0.0512 30 4.77696,-6.51264

512,0 31 0.7168,-2.54976

Lower Surface Lower Surface0

0.6748,-2.40036 1 482,04.49706,-6.13104 2 481.9759,-0.0241

11.18722,-10.42084 3 480.12984,0.1156820.35486,-15.15408 4 474.50972,0.313331.71078,-20.23918 5 465.17338,0.2602844.9465,-25.55082 6 452.36664,-0.3615

59.75354,-30.88656 7 436.4269,-1.783475.92464,-35.99094 8 417.78314,-4.1403893.32484,-40.71454 9 396.91736,-7.51438111.7035,-44.95132 10 374.35976,-11.88612130.76178,-48.4892 11 350.66464,-17.14956

150.32616,-51.03898 12 326.3622,-23.09744170.28096,-52.37412 13 301.96818,-29.45984190.58762,-52.25844 14 277.93566,-35.87044211.27024,-50.53288 15 254.67434,-41.91954232.48788,-47.02392 16 232.48788,-47.02392254.67434,-41.91954 17 211.27024,-50.53288277.93566,-35.87044 18 190.58762,-52.25844301.96818,-29.45984 19 170.28096,-52.37412326.3622,-23.09744 20 150.32616,-51.03898

350.66464,-17.14956 21 130.76178,-48.4892374.35976,-11.88612 22 111.7035,-44.95132396.91736,-7.51438 23 93.32484,-40.71454417.78314,-4.14038 24 75.92464,-35.99094

436.4269,-1.7834 25 59.75354,-30.88656452.36664,-0.3615 26 44.9465,-25.55082465.17338,0.26028 27 31.71078,-20.23918474.50972,0.3133 28 20.35486,-15.15408

480.12984,0.11568 29 11.18722,-10.42084

Page 26: NREL Phase VI - Test Blade & Aerofoil Geometry

481.9518,-0.0482 30 4.49706,-6.13104482,0 31 0.6748,-2.40036

Lower Surface Lower Surface0

0.6398,-2.27586 1 457,04.26381,-5.81304 2 456.97715,-0.02285

10.60697,-9.88034 3 455.22684,0.1096819.29911,-14.36808 4 449.89822,0.2970530.06603,-19.18943 5 441.04613,0.2467842.61525,-24.22557 6 428.90364,-0.3427556.65429,-29.28456 7 413.79065,-1.690971.98664,-34.12419 8 396.11389,-3.9256388.48434,-38.60279 9 376.33036,-7.12463

105.90975,-42.61982 10 354.94276,-11.26962123.97953,-45.9742 11 332.47664,-16.26006

142.52916,-48.39173 12 309.4347,-21.89944161.44896,-49.65762 13 286.30593,-27.93184180.70237,-49.54794 14 263.51991,-34.00994200.31224,-47.91188 15 241.46509,-39.74529220.42938,-44.58492 16 220.42938,-44.58492241.46509,-39.74529 17 200.31224,-47.91188263.51991,-34.00994 18 180.70237,-49.54794286.30593,-27.93184 19 161.44896,-49.65762309.4347,-21.89944 20 142.52916,-48.39173

332.47664,-16.26006 21 123.97953,-45.9742354.94276,-11.26962 22 105.90975,-42.61982376.33036,-7.12463 23 88.48434,-38.60279396.11389,-3.92563 24 71.98664,-34.12419413.79065,-1.6909 25 56.65429,-29.28456

428.90364,-0.34275 26 42.61525,-24.22557441.04613,0.24678 27 30.06603,-19.18943449.89822,0.29705 28 19.29911,-14.36808455.22684,0.10968 29 10.60697,-9.88034456.9543,-0.0457 30 4.26381,-5.81304

457,0 31 0.6398,-2.27586

Lower Surface Lower Surface0

0.6314,-2.24598 1 451,04.20783,-5.73672 2 450.97745,-0.02255

10.46771,-9.75062 3 449.25012,0.1082419.04573,-14.17944 4 443.99146,0.2931529.67129,-18.93749 5 435.25559,0.2435442.05575,-23.90751 6 423.27252,-0.3382555.91047,-28.90008 7 408.35795,-1.668771.04152,-33.67617 8 390.91327,-3.8740987.32262,-38.09597 9 371.38948,-7.03109

104.51925,-42.06026 10 350.28268,-11.12166122.35179,-45.3706 11 328.11152,-16.04658

140.65788,-47.75639 12 305.3721,-21.61192159.32928,-49.00566 13 282.54699,-27.56512

Page 27: NREL Phase VI - Test Blade & Aerofoil Geometry

178.32991,-48.89742 14 260.06013,-33.56342197.68232,-47.28284 15 238.29487,-39.22347217.53534,-43.99956 16 217.53534,-43.99956238.29487,-39.22347 17 197.68232,-47.28284260.06013,-33.56342 18 178.32991,-48.89742282.54699,-27.56512 19 159.32928,-49.00566305.3721,-21.61192 20 140.65788,-47.75639

328.11152,-16.04658 21 122.35179,-45.3706350.28268,-11.12166 22 104.51925,-42.06026371.38948,-7.03109 23 87.32262,-38.09597390.91327,-3.87409 24 71.04152,-33.67617408.35795,-1.6687 25 55.91047,-28.90008

423.27252,-0.33825 26 42.05575,-23.90751435.25559,0.24354 27 29.67129,-18.93749443.99146,0.29315 28 19.04573,-14.17944449.25012,0.10824 29 10.46771,-9.75062450.9549,-0.0451 30 4.20783,-5.73672

451,0 31 0.6314,-2.24598

Lower Surface Lower Surface0

0.588,-2.0916 1 420,03.9186,-5.3424 2 419.979,-0.0219.7482,-9.0804 3 418.3704,0.1008

17.7366,-13.2048 4 413.4732,0.27327.6318,-17.6358 5 405.3378,0.226839.165,-22.2642 6 394.1784,-0.315

52.0674,-26.9136 7 380.289,-1.55466.1584,-31.3614 8 364.0434,-3.607881.3204,-35.4774 9 345.8616,-6.547897.335,-39.1692 10 326.2056,-10.3572

113.9418,-42.252 11 305.5584,-14.9436130.9896,-44.4738 12 284.382,-20.1264148.3776,-45.6372 13 263.1258,-25.6704166.0722,-45.5364 14 242.1846,-31.2564184.0944,-44.0328 15 221.9154,-36.5274202.5828,-40.9752 16 202.5828,-40.9752221.9154,-36.5274 17 184.0944,-44.0328242.1846,-31.2564 18 166.0722,-45.5364263.1258,-25.6704 19 148.3776,-45.6372284.382,-20.1264 20 130.9896,-44.4738

305.5584,-14.9436 21 113.9418,-42.252326.2056,-10.3572 22 97.335,-39.1692345.8616,-6.5478 23 81.3204,-35.4774364.0434,-3.6078 24 66.1584,-31.3614

380.289,-1.554 25 52.0674,-26.9136394.1784,-0.315 26 39.165,-22.2642405.3378,0.2268 27 27.6318,-17.6358413.4732,0.273 28 17.7366,-13.2048

418.3704,0.1008 29 9.7482,-9.0804419.958,-0.042 30 3.9186,-5.3424

420,0 31 0.588,-2.0916

Page 28: NREL Phase VI - Test Blade & Aerofoil Geometry

Lower Surface Lower Surface0

0.5446,-1.93722 1 389,03.62937,-4.94808 2 388.98055,-0.019459.02869,-8.41018 3 387.49068,0.09336

16.42747,-12.23016 4 382.95494,0.2528525.59231,-16.33411 5 375.42001,0.2100636.27425,-20.62089 6 365.08428,-0.2917548.22433,-24.92712 7 352.22005,-1.439361.27528,-29.04663 8 337.17353,-3.3415175.31818,-32.85883 9 320.33372,-6.0645190.15075,-36.27814 10 302.12852,-9.59274105.53181,-39.1334 11 283.00528,-13.84062

121.32132,-41.19121 12 263.3919,-18.64088137.42592,-42.26874 13 243.70461,-23.77568153.81449,-42.17538 14 224.30907,-28.94938170.50648,-40.78276 15 205.53593,-33.83133187.63026,-37.95084 16 187.63026,-37.95084205.53593,-33.83133 17 170.50648,-40.78276224.30907,-28.94938 18 153.81449,-42.17538243.70461,-23.77568 19 137.42592,-42.26874263.3919,-18.64088 20 121.32132,-41.19121

283.00528,-13.84062 21 105.53181,-39.1334302.12852,-9.59274 22 90.15075,-36.27814320.33372,-6.06451 23 75.31818,-32.85883337.17353,-3.34151 24 61.27528,-29.04663352.22005,-1.4393 25 48.22433,-24.92712

365.08428,-0.29175 26 36.27425,-20.62089375.42001,0.21006 27 25.59231,-16.33411382.95494,0.25285 28 16.42747,-12.23016387.49068,0.09336 29 9.02869,-8.41018388.9611,-0.0389 30 3.62937,-4.94808

389,0 31 0.5446,-1.93722

Lower Surface Lower Surface0

0.5334,-1.89738 1 381,03.55473,-4.84632 2 380.98095,-0.019058.84301,-8.23722 3 379.52172,0.09144

16.08963,-11.97864 4 375.07926,0.2476525.06599,-15.99819 5 367.69929,0.2057435.52825,-20.19681 6 357.57612,-0.2857547.23257,-24.41448 7 344.97645,-1.409760.01512,-28.44927 8 330.23937,-3.2727973.76922,-32.18307 9 313.74588,-5.9397988.29675,-35.53206 10 295.91508,-9.39546103.36149,-38.3286 11 277.18512,-13.55598

118.82628,-40.34409 12 257.9751,-18.25752134.59968,-41.39946 13 238.69269,-23.28672150.65121,-41.30802 14 219.69603,-28.35402166.99992,-39.94404 15 201.30897,-33.13557183.77154,-37.17036 16 183.77154,-37.17036

Page 29: NREL Phase VI - Test Blade & Aerofoil Geometry

201.30897,-33.13557 17 166.99992,-39.94404219.69603,-28.35402 18 150.65121,-41.30802238.69269,-23.28672 19 134.59968,-41.39946257.9751,-18.25752 20 118.82628,-40.34409

277.18512,-13.55598 21 103.36149,-38.3286295.91508,-9.39546 22 88.29675,-35.53206313.74588,-5.93979 23 73.76922,-32.18307330.23937,-3.27279 24 60.01512,-28.44927344.97645,-1.4097 25 47.23257,-24.41448

357.57612,-0.28575 26 35.52825,-20.19681367.69929,0.20574 27 25.06599,-15.99819375.07926,0.24765 28 16.08963,-11.97864379.52172,0.09144 29 8.84301,-8.23722380.9619,-0.0381 30 3.55473,-4.84632

381,0 31 0.5334,-1.89738

Lower Surface Lower Surface0

0.5012,-1.78284 1 358,03.34014,-4.55376 2 357.9821,-0.01798.30918,-7.73996 3 356.61096,0.08592

15.11834,-11.25552 4 352.43668,0.232723.55282,-15.03242 5 345.50222,0.1933233.3835,-18.97758 6 335.99016,-0.2685

44.38126,-22.94064 7 324.1511,-1.324656.39216,-26.73186 8 310.30366,-3.0752269.31596,-30.24026 9 294.80584,-5.5812282.9665,-33.38708 10 278.05144,-8.8282897.12182,-36.0148 11 260.45216,-12.73764

111.65304,-37.90862 12 242.4018,-17.15536126.47424,-38.90028 13 224.28342,-21.88096141.55678,-38.81436 14 206.43354,-26.64236156.91856,-37.53272 15 189.15646,-31.13526172.67772,-34.92648 16 172.67772,-34.92648189.15646,-31.13526 17 156.91856,-37.53272206.43354,-26.64236 18 141.55678,-38.81436224.28342,-21.88096 19 126.47424,-38.90028242.4018,-17.15536 20 111.65304,-37.90862

260.45216,-12.73764 21 97.12182,-36.0148278.05144,-8.82828 22 82.9665,-33.38708294.80584,-5.58122 23 69.31596,-30.24026310.30366,-3.07522 24 56.39216,-26.73186

324.1511,-1.3246 25 44.38126,-22.94064335.99016,-0.2685 26 33.3835,-18.97758345.50222,0.19332 27 23.55282,-15.03242352.43668,0.2327 28 15.11834,-11.25552

356.61096,0.08592 29 8.30918,-7.73996357.9284,-0.0358 30 3.34014,-4.55376

358,0 31 0.5012,-1.78284

Tip TipLower Surface Lower Surface

0

Page 30: NREL Phase VI - Test Blade & Aerofoil Geometry

0.5012,-1.78284 1 358,03.34014,-4.55376 2 357.9821,-0.01798.30918,-7.73996 3 356.61096,0.08592

15.11834,-11.25552 4 352.43668,0.232723.55282,-15.03242 5 345.50222,0.1933233.3835,-18.97758 6 335.99016,-0.2685

44.38126,-22.94064 7 324.1511,-1.324656.39216,-26.73186 8 310.30366,-3.0752269.31596,-30.24026 9 294.80584,-5.5812282.9665,-33.38708 10 278.05144,-8.8282897.12182,-36.0148 11 260.45216,-12.73764

111.65304,-37.90862 12 242.4018,-17.15536126.47424,-38.90028 13 224.28342,-21.88096141.55678,-38.81436 14 206.43354,-26.64236156.91856,-37.53272 15 189.15646,-31.13526172.67772,-34.92648 16 172.67772,-34.92648189.15646,-31.13526 17 156.91856,-37.53272206.43354,-26.64236 18 141.55678,-38.81436224.28342,-21.88096 19 126.47424,-38.90028242.4018,-17.15536 20 111.65304,-37.90862

260.45216,-12.73764 21 97.12182,-36.0148278.05144,-8.82828 22 82.9665,-33.38708294.80584,-5.58122 23 69.31596,-30.24026310.30366,-3.07522 24 56.39216,-26.73186

324.1511,-1.3246 25 44.38126,-22.94064335.99016,-0.2685 26 33.3835,-18.97758345.50222,0.19332 27 23.55282,-15.03242352.43668,0.2327 28 15.11834,-11.25552

356.61096,0.08592 29 8.30918,-7.73996357.9642,-0.0358 30 3.34014,-4.55376

358,0 31 0.5012,-1.78284

Lower Surface Lower Surface0

0.4592,-1.63344 1 328,03.06024,-4.17216 2 327.9836,-0.01647.61288,-7.09136 3 326.72736,0.07872

13.85144,-10.31232 4 322.90288,0.213221.57912,-13.77272 5 316.54952,0.17712

30.586,-17.38728 6 307.83456,-0.24640.66216,-21.01824 7 296.9876,-1.213651.66656,-24.49176 8 284.30056,-2.8175263.50736,-27.70616 9 270.10144,-5.11352

76.014,-30.58928 10 254.75104,-8.0884888.98312,-32.9968 11 238.62656,-11.67024

102.29664,-34.73192 12 222.0888,-15.71776115.87584,-35.64048 13 205.48872,-20.04736129.69448,-35.56176 14 189.13464,-24.40976143.76896,-34.38752 15 173.30536,-28.52616158.20752,-31.99968 16 158.20752,-31.99968173.30536,-28.52616 17 143.76896,-34.38752189.13464,-24.40976 18 129.69448,-35.56176205.48872,-20.04736 19 115.87584,-35.64048

Page 31: NREL Phase VI - Test Blade & Aerofoil Geometry

222.0888,-15.71776 20 102.29664,-34.73192238.62656,-11.67024 21 88.98312,-32.9968254.75104,-8.08848 22 76.014,-30.58928270.10144,-5.11352 23 63.50736,-27.70616284.30056,-2.81752 24 51.66656,-24.49176

296.9876,-1.2136 25 40.66216,-21.01824307.83456,-0.246 26 30.586,-17.38728

316.54952,0.17712 27 21.57912,-13.77272322.90288,0.2132 28 13.85144,-10.31232

326.72736,0.07872 29 7.61288,-7.09136327.9672,-0.0328 30 3.06024,-4.17216

328,0 31 0.4592,-1.63344

Lower Surface Lower Surface0

0.427,-1.5189 1 305,02.84565,-3.8796 2 304.98475,-0.015257.07905,-6.5941 3 303.8166,0.0732

12.88015,-9.5892 4 300.2603,0.1982520.06595,-12.80695 5 294.35245,0.164728.44125,-16.16805 6 286.2486,-0.2287537.81085,-19.5444 7 276.16225,-1.128548.0436,-22.77435 8 264.36485,-2.6199559.0541,-25.76335 9 251.1614,-4.7549570.68375,-28.4443 10 236.8874,-7.521382.74345,-30.683 11 221.8936,-10.8519

95.1234,-32.29645 12 206.5155,-14.6156107.7504,-33.1413 13 191.07945,-18.6416

120.60005,-33.0681 14 175.87215,-22.6981133.6876,-31.9762 15 161.15285,-26.52585147.1137,-29.7558 16 147.1137,-29.7558

161.15285,-26.52585 17 133.6876,-31.9762175.87215,-22.6981 18 120.60005,-33.0681191.07945,-18.6416 19 107.7504,-33.1413206.5155,-14.6156 20 95.1234,-32.29645221.8936,-10.8519 21 82.74345,-30.683236.8874,-7.5213 22 70.68375,-28.4443

251.1614,-4.75495 23 59.0541,-25.76335264.36485,-2.61995 24 48.0436,-22.77435276.16225,-1.1285 25 37.81085,-19.5444286.2486,-0.22875 26 28.44125,-16.16805294.35245,0.1647 27 20.06595,-12.80695300.2603,0.19825 28 12.88015,-9.5892303.8166,0.0732 29 7.07905,-6.5941304.9695,-0.0305 30 2.84565,-3.8796

305,0 31 0.427,-1.5189

Page 32: NREL Phase VI - Test Blade & Aerofoil Geometry

0.00 0.05 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.00

-0.15

-0.10

-0.05

0.00

0.05

0.10

0.15

Page 33: NREL Phase VI - Test Blade & Aerofoil Geometry

0.000222 0.0004440.000556 -0.0022280.000794 -0.0030280.001028 -0.0036780.001267 -0.0042560.001506 -0.0047560.001744 -0.0052220.001967 -0.0056220.002222 -0.0060440.002472 -0.006456

0.0027 -0.0067940.002956 -0.0071720.003189 -0.0074940.003433 -0.0078110.003689 -0.0081220.00395 -0.008444

0.004172 -0.0086890.004444 -0.0089780.004717 -0.0092940.00495 -0.009544

0.005189 -0.0097610.005494 -0.0100780.00575 -0.010339

0.006 -0.0105780.006289 -0.0108440.006572 -0.0111390.006789 -0.0113440.007017 -0.0115280.007339 -0.0118060.007622 -0.0120610.007883 -0.0123060.008094 -0.0124780.008372 -0.01270.008656 -0.0129330.008906 -0.0131330.009139 -0.0133110.009717 -0.0137780.010217 -0.0141220.010789 -0.0145670.011311 -0.0149610.011822 -0.0153280.012339 -0.015672

0.0129 -0.0160610.013422 -0.016450.013911 -0.0167440.014489 -0.0171670.014956 -0.017450.015528 -0.0178220.016056 -0.0181780.016567 -0.0184890.017128 -0.018850.017656 -0.0192060.018156 -0.01950.018722 -0.019844

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

-0.15

-0.1

-0.05

0

0.05

0.1

0.15

Page 34: NREL Phase VI - Test Blade & Aerofoil Geometry

0.019272 -0.0201940.019783 -0.020522

0.0203 -0.02080.020878 -0.0211940.021339 -0.0214280.021944 -0.0217940.022456 -0.0221170.022944 -0.0223610.023544 -0.0227170.024067 -0.023050.024556 -0.0232890.025156 -0.0236780.025606 -0.02390.026194 -0.0242440.026706 -0.02450.027278 -0.0248440.027744 -0.0250440.028383 -0.0254110.028894 -0.0257170.029383 -0.0259330.029983 -0.0262780.030489 -0.0265390.031039 -0.0268390.031572 -0.0271170.032106 -0.0273890.03265 -0.027667

0.033194 -0.027950.033711 -0.0282060.034272 -0.0284890.034783 -0.0287440.035317 -0.0290.035872 -0.0292780.036422 -0.0295560.036944 -0.0298330.037433 -0.0300390.038056 -0.0303330.038622 -0.0306560.039089 -0.0308610.039656 -0.0311280.040194 -0.0313780.040778 -0.0316560.041311 -0.0319280.041783 -0.0321220.042372 -0.0324170.042889 -0.0326670.043456 -0.0329170.043989 -0.0331720.044533 -0.0334330.045078 -0.0336780.045606 -0.0339220.04615 -0.034167

0.046717 -0.0344220.047244 -0.0346780.047772 -0.034922

Page 35: NREL Phase VI - Test Blade & Aerofoil Geometry

0.048328 -0.0351610.048844 -0.0353940.049411 -0.0356560.049961 -0.0359060.050483 -0.036150.051039 -0.03640.051567 -0.0366330.052061 -0.036850.063189 -0.0416890.074267 -0.0462720.085333 -0.050650.096417 -0.0547890.107494 -0.0588060.118578 -0.0626390.129667 -0.0663780.140739 -0.0698780.151828 -0.0732440.162917 -0.076428

0.174 -0.0795280.185083 -0.0824390.196178 -0.0852280.207267 -0.0878780.21835 -0.090417

0.229439 -0.0927720.240533 -0.0950280.251617 -0.0971170.262706 -0.0990330.273789 -0.1007890.284878 -0.1023890.295978 -0.1038390.307061 -0.1050830.318156 -0.1061560.329261 -0.1070720.340344 -0.1077560.351439 -0.1082440.362539 -0.1085390.373622 -0.1086280.384744 -0.108450.395822 -0.1080440.406922 -0.1074170.418039 -0.1065440.429133 -0.105450.440244 -0.1041440.451339 -0.1026060.46245 -0.100861

0.473567 -0.0989060.484689 -0.096750.495806 -0.0944170.506939 -0.0919280.518067 -0.089322

0.5292 -0.0866060.540333 -0.0838280.551478 -0.080978

0.5626 -0.0781

Page 36: NREL Phase VI - Test Blade & Aerofoil Geometry

0.573767 -0.0751560.584906 -0.0722060.596028 -0.0692440.607189 -0.0662780.618311 -0.0633220.62945 -0.060350.6406 -0.0574

0.651728 -0.0544720.662867 -0.0515720.674028 -0.0486940.685161 -0.0458440.696311 -0.0430170.707456 -0.0402560.718594 -0.0375610.729728 -0.0349330.740878 -0.0323220.752006 -0.0297830.763144 -0.0273110.774278 -0.0249330.785406 -0.0226390.796556 -0.0204280.807683 -0.0182780.818817 -0.0162170.829967 -0.01430.841089 -0.01250.852233 -0.0107830.863372 -0.0091670.90545 -0.00370.93852 -0.000750.96509 0.000540.98446 0.000650.99612 0.00024

1 00.99623 0.000540.98528 0.002450.96799 0.0060.94523 0.011010.91763 0.01694

0.874572 0.0255390.863456 0.0275940.852344 0.0296220.841244 0.031650.830133 0.0336940.819028 0.035750.807922 0.0378280.796817 0.0398940.785706 0.0419720.774594 0.0440670.763483 0.0461720.752383 0.0482830.741261 0.0503940.730128 0.0524890.719017 0.0545890.707889 0.056706

0.93 0.94 0.95 0.96 0.97 0.98 0.99 1 1.01

-0.002

0

0.002

0.004

0.006

0.008

0.01

0.012

Column B

Page 37: NREL Phase VI - Test Blade & Aerofoil Geometry

0.696767 0.0588220.685644 0.0609390.674517 0.0630670.663389 0.0652060.652278 0.067350.641156 0.0695060.630056 0.0716560.618939 0.0737940.607822 0.0759280.596717 0.0780720.585611 0.080183

0.5745 0.0817720.563389 0.0844280.552294 0.0864720.541161 0.0884670.530072 0.0904170.518961 0.0922670.507861 0.0940.496789 0.095550.485683 0.0969060.474589 0.0980830.463517 0.0990670.452417 0.0998780.441328 0.1004780.430244 0.1008830.419133 0.10110.408039 0.1011890.396939 0.101150.385807 0.1009830.374744 0.1006940.363639 0.1003280.352533 0.0998720.341433 0.0993440.330328 0.0987060.319217 0.0979780.308122 0.0971390.297006 0.0961890.285911 0.0951330.274806 0.0939560.263694 0.0926670.252594 0.0912780.241483 0.0897780.230367 0.0881830.219267 0.0864780.20815 0.08465

0.197044 0.0827220.18595 0.080656

0.174822 0.078450.163728 0.0760890.152617 0.0736060.141494 0.0709170.130389 0.0680670.119278 0.0650940.108156 0.061922

Page 38: NREL Phase VI - Test Blade & Aerofoil Geometry

0.09705 0.0584890.085939 0.0548170.074828 0.0508390.063728 0.0465280.052572 0.0418330.052083 0.0416220.05155 0.041367

0.050983 0.0411220.050433 0.0408830.049922 0.0406330.04935 0.040383

0.048789 0.0401440.048278 0.0399170.047717 0.0396670.047189 0.0394330.046639 0.039189

0.0461 0.0389440.045578 0.0387060.045039 0.0384390.044511 0.0381780.043956 0.0379110.043417 0.0376390.042878 0.0373560.042267 0.0370610.041811 0.0368670.041256 0.0365830.040694 0.03630.040161 0.0360330.039633 0.0357780.039078 0.0354780.038511 0.03520.037989 0.0349330.037456 0.0346440.036889 0.0343390.036339 0.0340830.035856 0.0338330.035244 0.0334780.034761 0.0332670.034222 0.0329440.033667 0.032650.033144 0.0323670.032606 0.0320610.032067 0.0317720.031556 0.0314830.030956 0.0311390.030489 0.03090.029883 0.0305110.029394 0.0302610.028867 0.029928

0.0283 0.0295890.027767 0.0292720.027228 0.028950.026661 0.02860.02615 0.028306

Page 39: NREL Phase VI - Test Blade & Aerofoil Geometry

0.025639 0.0279720.025039 0.0275720.024528 0.0272830.024011 0.0269390.023467 0.0265830.022944 0.0262330.022372 0.0258560.021872 0.0255560.02135 0.025183

0.020767 0.0247890.020267 0.0244720.019744 0.0240890.019206 0.0237060.018689 0.0233280.018111 0.02290.017617 0.022550.017089 0.0221390.01655 0.021717

0.016006 0.02130.015489 0.0209110.014956 0.0204780.014417 0.0200560.013889 0.0196220.013356 0.0191830.012817 0.0187330.012283 0.0182830.011722 0.0178110.011211 0.0173830.010667 0.0168940.010111 0.0164060.009628 0.015950.009328 0.0156330.009044 0.0153720.008806 0.0151440.008522 0.014850.008261 0.0146060.007972 0.01430.007728 0.0140560.007456 0.013750.007167 0.013450.006922 0.0131940.00665 0.012878

0.006383 0.0125780.006122 0.0122890.005867 0.0119940.005589 0.0116610.005328 0.011350.005056 0.0110170.004806 0.0107110.004544 0.0103720.004272 0.0100330.004033 0.0097110.003767 0.0093330.003522 0.009006

Page 40: NREL Phase VI - Test Blade & Aerofoil Geometry

0.003278 0.0086390.003011 0.0082280.002767 0.0078440.002517 0.0074220.002283 0.0070390.002033 0.0065890.001778 0.00610.001539 0.005628

0.0013 0.0050830.001056 0.0045060.000817 0.0038670.000583 0.0030720.00025 0.001172

0.000222 0.000444

Page 41: NREL Phase VI - Test Blade & Aerofoil Geometry

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

-0.15

-0.1

-0.05

0

0.05

0.1

0.15

Page 42: NREL Phase VI - Test Blade & Aerofoil Geometry

0.93 0.94 0.95 0.96 0.97 0.98 0.99 1 1.01

-0.002

0

0.002

0.004

0.006

0.008

0.01

0.012

Column B

Page 43: NREL Phase VI - Test Blade & Aerofoil Geometry

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

-0.15

-0.1

-0.05

0

0.05

0.1

0.15


Recommended